| 1. | Precise integration for control law of optimal tracking
跟踪问题最优控制律精细积分 |
| 2. | By duality approach , we characterize the optimal control law
并用对偶方法刻画了最优控制律的特征 |
| 3. | Optimal control law
最优控制律 |
| 4. | A full - dimension state predictive observer for discrete system with control time - delay is first structured
所以，完全可以根据无时滞系统来设计最优控制律。 |
| 5. | By using successive approximation approach , the feedforward and feedback optimal control law is presented , and a disturbance observer is designed to make the optimal controller physically realizable
采用逐次逼近算法给出了系统前馈反馈最优控制律的设计方法，利用扰动观测器解决了最优控制律的物理可实现问题。 |
| 6. | The order - reduced results are verified by comparing the zeros , poles and outputs curves before and after the order reduction and applying the linear quadratic optimal control law for low - order model to the high - order model
通过零极点比较、输出曲线比较和将针对低阶模型设计的线性二次型最优控制律加入原高阶模型等方法对降阶结果进行了验证。 |
| 7. | Designed semi - physical simulations emphasized on attitude determination algorithm based on star sensor combined with gyroscope , bang - off - bang time - optimal jet control algorithm , and quaternion feedback control algorithm using flywheel
重点针对星敏感器和速率陀螺联合定姿算法、喷气bang - off - bang时间最优控制律算法、反作用飞轮四元数反馈稳态控制律算法分别设计了半物理仿真实验。 |
| 8. | First we identify the controlled plant offline , when the precision reaches a certain extent , we will achieve recursive predictive model by on - line identification . finally we acquire the optimized control law by minimizing the function of performance guideline
首先对被控对象进行离线辨识，在模型辨识达到一定的精度后，再在线递推得到预测模型，最后通过极小化性能指标得到最优控制律。 |
| 9. | These controllers demonstrate effective performances by numerical simulations . the simulations also indicate that the system track the reference trajectories well under the control of trajectory track control laws . in the end , an experimental apparatus for tethered mass system is utilized to
数值仿真表明,线性二次型最优控制律对系统的面内和面外运动均具有良好的控制效果,在参考轨迹控制中系统能较好地追踪参考轨迹。 |
| 10. | The attitude control system using reaction thrusters is studied . based on phase plane theory , pd control law , time - optimal control law and time - fuel optimal control law were designed . characteristics and application conditions of these laws were compared in simulations
针对以喷气推力器作为执行机构的姿态控制系统,基于相平面分析方法,分别设计了pd 、时间最优和燃料-时间混合最优控制律,在仿真中分别比较了这几种方法的特点和适用条件。 |
